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aerodynamic center aerodynamic characteristics aileron deflection airfoil contour airfoil section angle of attack bend location bending the cover central location change in vent chord climb combination Committee for Aeronautics cooling-air flow cover plates curves cylinder density altitude downrigged ailerons drag coefficient effective nacelle drag engine expedite general distribution fan or cuffs figures l5 fillets flap deflection flap hinge flight fuselage high-speed inches increment indicated airspeed induced drag interference drag internal balance investigation l6-inch nacelle Langley Memorial Aeronautical maximum lift coefficient Memorial Aeronautical Laboratory miles per hour modified cowl flaps nacelle diameter nacelle-propeller National Advisory Committee negative tabs notch obtained percent positive tabs propeller operating propulsive thrust ratio root chord Short-nose low-inlet-velocity cowling shown in figure specimen stick forces stress concentration thickness tho wing tion tl tl trailing edge True Airspeed variation vent width WARTIME REPORT ORIGINALLY wind tunnel wing-fuselage wing-nacelle XP-42 airplane